Sökresultat

LES of Supersonic Combustion in a Mach 2 Cavity-Based Model Scramjet Combustor with Conjugate Heat Transfer and Radiative Heat Transfer

Le: A procedural marker in Mandarin Chinese

LES of supersonic combustion in a scramjet engine model

Comparison of LES Models Applied to a Bluff Body Stabilized Flame

The Core and Specifics of Mandarin Chinese marker le: A unified approach and a Cognitive Grammar representation

LES of Stable Combustion and Lean Blow-out in a Mach 2 Cavity Flameeholder

The facsimile of The Rudiments or Principles of the German flute : the first English translation of Principes de la Flute Traversiere ou Flute d’Allemagne (1707) by Jacques Hotteterre Le Romain

Taking Issue With Le Poidevin's New Agnosticism

LES of Combustion Dynamics in an Ethylene-Hydrogen-Air Ramjet

LES/FGM investigation of ignition and flame structure in a gasoline partially premixed combustion engine

LES of H₂-air jet combustion in high enthalpy supersonic crossflow

Combustion LES of a multi-burner annular aero-engine combustor using a skeletal reaction mechanism for jet- a air mixtures

In this study we describe combustion simulations of a single sector and a fully annular generic multi-burner aero-engine combustor. The objectives are to facilitate the understanding of the flow, mixing and combustion processes to help improve the combustor design and the design process, as well as to show that it is now feasible to perform high-fidelity reacting flow simulations of full annular g

Short- and long-time diffusion and dynamic scaling in suspensions of charged colloidal particles

Swirl stabilized premixed flame analysis using of LES and POD

For environmental and human health reasons, the regulations on the emissions from combustion devices are getting more and more strict. In particular, it is important to abate the emission of pollutants deriving from combustion in gas turbines. A solution is the use of swirl stabilized, lean premixed combustion. Besides the beneficial effects, there are still some issues related to instabilities an

LES of swirling flows in gas turbine combustion chambers

Climate-driven changes in lake conditions during late MIS 3 and MIS 2: a high-resolution geochemical record from Les Echets, France

A Comparative Study of LES Turbulent Combustion Models Applied to a Low Swirl Lean Premixed Burner

Measurements and LES of a SGT-800 Burner in a Combustion Rig

The Siemens gas turbine SGT-800 is the largest industrial gas turbine produced by Siemens Industrial Turbomachinery (SIT) offering a dry low emission (DLE) capability below 15 ppm NOx. It has a very high reliability using an annular combustor system with passive damping and 30 DLE burners. To obtain a greater understanding of the mixing process and the flame dynamics and in order to further reduce

LES Modeling of the DLR Generic Single-Cup Spray Combustor : Validation and the Impact of Combustion Chemistry

le Critérion (e56), for woodwind quartet (fl, ob, cl, bsn)